Airframe Structural Components: 2-23277-5, 2-23285-10, 2-23316-5
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2-23277-5 2232775 | 1560-00-709-3702 | Flap Hinge, Aileron | General Characteristics Item Description: Aluminum alloy Criticality Code Justification: TEXT | A R Machine Inc. (59784) Flight Materials (0XB66) GKN Aerospace Bandy Machining Inc. (22176) Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) Tect Aerospace Inc. (34336) | |
| 2-23277-6 2232776 | 1560-00-709-7218 | Flap Hinge, Aileron | General Characteristics Item Description: Aluminum alloy | Derco Aerospace Inc. (8X044) First Flight Co. (1K3G1) Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23278-7 2232787 | 1560-00-767-9567 | Flap Hinge, Aileron | General Characteristics Item Description: CRES | Aerometals Inc. (32664) Aeroparts Manufacturing & Repair Inc. (15992) Aircraft Hinge Inc. (0CD56) GKN Aerospace Bandy Machining Inc. (22176) Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) Smiley Industries Inc. (30507) Tect Aerospace Inc. (34336) | |
| 2-23278-8 2232788 | 1560-00-767-9568 | Flap Hinge, Aileron | General Characteristics Item Description: CRES | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23285-10 22328510 | 1560-00-447-8978 | Panel, Wing | General Characteristics Item Description: Aluminum 7075-0 QQ-A-287 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23285-14 22328514 | 1560-00-447-8978 | Panel, Wing | General Characteristics Item Description: Aluminum 7075-0 QQ-A-287 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23288-1 2232881 | 1560-00-447-8980 | Panel, Structural, Aircraft | Aircraft Mission Design Series: T-38 Special Features: Matl: alum alloy; permissible to bond honeycomb core and skin panel in the flat Aircraft Location: WING | Northrop Grumman Systems Corporation (76823) | |
| 2-23288-2 2232882 | 1560-00-447-8981 | Panel Assembly, Wing | General Characteristics Item Description: Aluminum alloy | Northrop Grumman Systems Corporation (76823) | |
| 2-23288-501 223288501 | 1560-00-447-8980 | Panel, Structural, Aircraft | Aircraft Mission Design Series: T-38 Special Features: Matl: alum alloy; permissible to bond honeycomb core and skin panel in the flat Aircraft Location: WING | Northrop Grumman Systems Corporation (76823) | |
| 2-23288-502 223288502 | 1560-00-447-8981 | Panel Assembly, Wing | General Characteristics Item Description: Aluminum alloy | Northrop Grumman Systems Corporation (76823) | |
| 2-23290-1 2232901 | 1560-00-137-3793 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/12 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23291-1 2232911 | 1560-00-137-3795 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/12 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23291-2 2232912 | 1560-00-137-3796 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/12 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23292-2 2232922 | 1560-00-139-0841 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/12 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23292-3 2232923 | 1560-00-137-3788 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/12 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 223-31167-13 2233116713 | 1560-00-446-5620 | Longeron | Boeing Company, The (43999) | ||
| 223-311903-361 223311903361 | 1560-00-431-9756 | Fuselage Section | Boeing Company, The (43999) | ||
| 2-23313-1 2233131 | 1560-00-767-9576 | Bushing, Actuation, Main Landing g | III End Item Identification: Aircraft model T38 General Characteristics Item Description: Aluminum bronze, MIL-B-6946, 0.938 in. min, 0.939 in. max od of body, 0.455 in. min, 0.465 in. max lg of body, 1.120 in. min, 1.130 in. max dia of flg, 0.811 in. min, 0.812 in. max spherical radius of flanged end, 0.750 in. min, 0.751 in. max id, cadmium plated finish except id and spherical radius | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23316-1 2233161 | 1560-00-909-8338 | Spar, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-367 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23316-5 2233165 | 1560-00-139-0847 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-367 T6 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) |